Beispiel #1
0
 /// <summary>
 /// 默认构造函数。当前时刻的运动状态。
 /// </summary>
 /// <param name="MeanAnomaly">本时刻卫星的平近点角,弧度</param>
 /// <param name="PlaneEllipse">椭圆轨道</param>
 public MomentEllipseOrbit(double MeanAnomaly, PlaneEllipse PlaneEllipse)
 {
     this.PlaneEllipse = PlaneEllipse;
     this.MeanAnomaly  = MeanAnomaly;
 }
Beispiel #2
0
 /// <summary>
 /// 默认构造函数。当前时刻的运动状态。
 /// </summary>
 /// <param name="MeanAnomaly">参考时刻τ卫星的平近点角,弧度</param>
 /// <param name="deltaTime">与参考时刻之差</param>
 /// <param name="PlaneEllipse">椭圆轨道</param>
 public MomentEllipseOrbit(double MeanAnomaly, double deltaTime, PlaneEllipse PlaneEllipse)
     : this(MeanAnomaly + PlaneEllipse.MeanAngularVelocity * deltaTime, PlaneEllipse)
 {
 }